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propellant space propulsion systems. A significant limiting factor of hybrid propulsion systems is the continuous change in surface area of the propellant grain during the combustion process. This changing O/F
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no less than 5.5 in each component test area) or equivalent. The studentship is supported for 3.5 years and includes full Home tuition fees plus a stipend of £20,780 per annum 2025/26 rate (UKRI). The
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adverse consequences for overall thermal efficiency and component life (environmental impact, sustainability and safety). While standard analytical models for heat transfer exist for classical cases
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will dynamically adjust turbine parameters such as yaw, pitch, and torque to maximize Annual Energy Production (AEP) while minimizing component stress. Additionally, a hybrid predictive maintenance model
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models used in component scale CFD assessments. In particular, this concerns quantifying the effects of the heat transfer surface’s detailed topography, porosity and wettability on near-wall bubble
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: The student will gain knowledge in plant nutrition, metal toxicity and mycorrhizal symbiosis. The student will learn how to successfully maintain a growth experiment and will be supported during data analyses
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temperatures. This phenomenon is known as “Hot Corrosion”, also called high-temperature corrosion. In other words, the formation of a permeable non-protective oxide film at metal or alloy surface having
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the Project element or equivalent with a minimum 60% overall module average. the potential to engage in innovative research and to complete the PhD within a three-year period of study. a minimum of English
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Guidelines we are seeking to appoint a candidate with a strong profile of relevant qualitative research interests and training (i.e. preferably relating to elements of investigative methods), ideally with
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accelerated in the last few years along with the booming of digital technologies. One of the key elements for a successful implementation of the PdM strategy is the usage of technologies that can effectively